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180results about How to "Improve forwarding speed" patented technology

Multi-protocol industrial communication safety gateway and communication method with gateway applied

The invention relates to a multi-protocol industrial communication safety gateway and a communication method with the gateway applied. In the data communication process, a source gateway encrypts data through a secret key management mechanism module and a VPN encryption and decryption module and then sends the data to a target gateway. The target gateway decrypts the data through the VPN encryption and decryption module, and provides safe detection and control service for data communication through a safety domain safety protection module; if the data are safe, secret key decryption is carried out on application layer data, the types of the application layer data are judged, an application management safety module is used for management if the application layer data are application management data, and an application layer message detecting and filtering module is called for detecting and filtering messages if the application layer data are application layer messages. The mode of combination of the VPN encryption and decryption, the secret key encryption and decryption, and the application layer message detecting and filtering is adopted for communication safety assurance; the safety domain safety protection and the application safety management are adopted for gateway application safety assurance.
Owner:山东华汉电子有限公司

Message forwarding method and message forwarding device

InactiveCN103237039ASolve the problem of large resource consumption and low forwarding efficiencySolve the problem of high consumption and low forwarding efficiencyData switching networksMessage forwardingCentral processing unit
The invention provides a message forwarding method and a message forwarding device. The method comprises the following steps: receiving a message to be forwarded by a network device, and acquiring a 5-tuple group; finding out whether a message forwarding session table matched with the 5-tuple group exists in the existing message forwarding session tables, if so, processing the message to be forwarded through a processing manner recorded in the matched message forwarding session table, and transmitting the processed message; if not, finding out whether a blacklist session table matched with the 5-tuple group exists in the existing blacklist session tables, if so, discarding the message to be forwarded, and if not, processing the message to be forwarded by the network device; if the message to be forwarded is processed and successfully transmitted, establishing the message forwarding session table of the 5-tuple group; recording the processing manner into the message forwarding session table; if the message to be forwarded is discarded by any one module in processing, establishing the blacklist session table of the 5-tuple group; and recording a discarding module and discarding reasons into the blacklist session table. With the adoption of the message forwarding method and the message forwarding device, CPU (central processing unit) consumption can be reduced, and the forwarding efficiency is improved.
Owner:OPZOON TECH

Packet routing switch device and method thereof

The invention relates to network communication technology, in particular to a message routing and switching technique in wide-area network communication. A message routing and switching device comprise a host CPU, a three-layered switching unit, and a wide-area network sub-card. The host CPU obtains and maintains a first mapping relation and a second mapping relation, and respectively transmits to the three-layered switching unit and the wide-area network sub-card; the three-layered switching unit, after receiving the message, searches the first mapping relation and obtains virtual channel identification information, and transmitting the message to the wide-area network sub-card when the virtual channel identification information is added to the message; the wide-area network sub-card, after receiving the message, searches the second mapping relation and obtains a corresponding wide-area network interface virtual channel number, and transmits the message to the corresponding wide-area network interface virtual channel. In addition, the invention also provides a message routing and switching method. In the invention, the wide-area network sub-card assists the three-layered switching chip to replace the host CPU to carry out message retransmission in the wide-area network, so as to improve the speed of message retransmission.
Owner:RUIJIE NETWORKS CO LTD

Combined type tilting rotor-wing helicopter

The invention discloses a combined type tilting rotor-wing helicopter. The aircraft has characteristics of vertical ascending and descending, hovering and high-speed forward flight; compared with a traditional helicopter, the flight speed is high; compared with a tilting rotor-wing aircraft, the control reliability is high. The aircraft comprises a main lifting power rotor wing, a tilting rotor wing, a tilting airfoil, a fixed airfoil, a fuselage body and an undercarriage. The main lifting power rotor wing is a coaxial reversing propeller double-rotor-wing system; the tilting rotor wing and the tilting airfoil can be rotated through an actuating mechanism along a rotary shaft. The aircraft needs to undergo a vertical flight state, a transition flight state and a vertical flight state from takeoff to flat flight. In a whole flight process, the main lifting power rotor wing provides main lifting power to the aircraft all the time, and attitude of the aircraft is mainly controlled through tilting of the tilting rotor wing and the tilting airfoil. The combined type tilting rotor-wing helicopter has advantages of the tilting rotor wing and a coaxial helicopter, and mechanism and control defects of the tilting rotor wing and the coaxial helicopter are overcome; meanwhile, the reliability of the mechanism and a control method is improved.
Owner:北京天宇新超航空科技有限公司

Solid pulse plasma thruster with high propellant utilization rate and working method

The invention discloses a solid pulse plasma thruster with high propellant utilization rate and a working method, and belongs to the technical field of aerospace propulsion of micro-satellites. The solid pulse plasma thruster with high propellant utilization rate comprises a constant-force spring, an upper insulating plate for fixing a propellant, a semiconductor spark plug, a permanent magnet for increasing impulse bit, a cathode plate, a permanent magnet for increasing specific impulse, an anode plate, a high-voltage power supply, a main spark-gap capacitor, a diode, a lower insulating plate for fixing the propellant and a solid propellant; gas storage cavities for reducing the forward movement speed of neutral gas are respectively formed in the cathode plate and the anode plate; the distance between the cathode plate and the anode plate is increased on the rear sides of the gas storage cavities; tail ends, which are close to a nozzle, of the cathode plate and the anode plate are parallel to each other; the permanent magnet for increasing the impulse bit is added in the direction which is opposite to the direction of a self-inductance magnetic field; and the permanent magnet for increasing the specific impulse is added in the direction which is the same as the direction of the self-inductance magnetic field. The propellant utilization rate of the solid pulse plasma thruster can be increased. The solid pulse plasma thruster has the advantage of low cost, and is suitable for being used as a main thruster of a micro-nano satellite or an adjusting device of various large satellites.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Industrial SDN network data transmission method and system capable of supporting packet header compression

The invention discloses an industrial SDN network data transmission method and system capable of supporting packet header compression. The method includes: in a transmission preparation stage, an edge switch receives and forwards data to a controller, and the controller distributes an identifier ID for non-real-time data and sends a distribution result to a switch on a transmission path in the format of a flow table; and in a data transmission stage, the edge switch directly performs forwarding operation on real-time data, performs packet header compression/decompression on the non-real-time data, and forwards the data after a packet header adds/removes the identifier ID. A core switch matches the real-time data with L2 layer packet header information, matches the identifier ID with the non-real-time data, and forwards the data according to a matching flow table. The system comprises a controller and a switch capable of realizing functions of compression/decompression of the data packet header and identifier adding/removing. According to the method and system, the bandwidth cost can be reduced, the data forwarding speed can be increased, the data transmission efficiency is improved, more network resources are reserved for real-time data transmission of an industrial network, and the overall transmission performance of the industrial network is enhanced.
Owner:SHENYANG INST OF AUTOMATION - CHINESE ACAD OF SCI

Multi-rotor aircraft

The invention relates to a multi-rotor aircraft, which comprises four main rotor systems, two auxiliary rotor systems, a body and a flying integrated system arranged in the body, wherein an original point of a coordinate system of the body is the gravity center of the aircraft; a z axis is vertical upwards; an x axis is vertical to the z axis and points to the front part; a y axis is determined by a right-hand rule; the four main rotor systems are respectively distributed inside four quadrants of an x-y plane of the body coordinate system; each rotary axis of the four main rotor systems and the z axis of the body coordinate system form an included angle theta, and a projection of each rotary axis on an x-o-y plane of the body coordinate system is overlapped with the projection of a connection line from a rotation center to the original point of the body coordinate system on the x-o-y plane of the body coordinate system. According to the invention, movement and gesture change of the aircraft can be achieved by adjusting rotating speed of the four main rotor systems and the two auxiliary rotor systems; and the aircraft can achieve the actions such as vertical take-off and landing, forward flying, reverse flying, hovering, rolling and the like, and the stability and the controllabitity are good.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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